001444862 000__ 03862cam\a2200577Ii\4500 001444862 001__ 1444862 001444862 003__ OCoLC 001444862 005__ 20230310003731.0 001444862 006__ m\\\\\o\\d\\\\\\\\ 001444862 007__ cr\cn\nnnunnun 001444862 008__ 220305s2022\\\\sz\a\\\\ob\\\\001\0\eng\d 001444862 019__ $$a1301945163$$a1302001163$$a1302106853$$a1302127761$$a1302183649$$a1302236565$$a1302319671 001444862 020__ $$a9783030897581$$q(electronic bk.) 001444862 020__ $$a3030897583$$q(electronic bk.) 001444862 020__ $$z9783030897574 001444862 020__ $$z3030897575 001444862 0247_ $$a10.1007/978-3-030-89758-1$$2doi 001444862 035__ $$aSP(OCoLC)1302007639 001444862 040__ $$aEBLCP$$beng$$erda$$epn$$cEBLCP$$dYDX$$dGW5XE$$dOCLCO$$dOCLCF$$dN$T$$dUKAHL$$dOCLCQ 001444862 049__ $$aISEA 001444862 050_4 $$aQB603.M6$$bL66 2022 001444862 08204 $$a521/.3$$223 001444862 1001_ $$aLonguski, Jim,$$eauthor. 001444862 24510 $$aIntroduction to orbital perturbations /$$cJames M. Longuski, Felix R. Hoots, George E. Pollock IV. 001444862 264_1 $$aCham :$$bSpringer,$$c[2022] 001444862 264_4 $$c©2022 001444862 300__ $$a1 online resource (349 pages) :$$billustrations (some color). 001444862 336__ $$atext$$btxt$$2rdacontent 001444862 337__ $$acomputer$$bc$$2rdamedia 001444862 338__ $$aonline resource$$bcr$$2rdacarrier 001444862 4901_ $$aSpace technology library ;$$vvolume 40 001444862 504__ $$aIncludes bibliographical references and index. 001444862 5050_ $$aChapter 1. The n-Body Problem -- Chapter 2. General Perturbations -- Chapter 3. Evaluation of Lagranges Brackets -- Chapter 4. Lagranges Planetary Equations -- Chapter 5. Expansion of the Perturbation Function -- Chapter 6. The Earth-Moon System -- Chapter 7. Potential of an Oblate Spheroid -- Chapter 8. Effects of General Relativity -- Chapter 9. Perturbations due to Atmospheric Drag -- Chapter 10. Periodic Solutions in Nonlinear Oscillations. 001444862 506__ $$aAccess limited to authorized users. 001444862 520__ $$aThis textbook provides details of the derivation of Lagrange's planetary equations and of the closely related Gauss's variational equations, thereby covering a sorely needed topic in existing literature. Analytical solutions can help verify the results of numerical work, giving one confidence that his or her analysis is correct. The authorsall experienced experts in astrodynamics and space missionstake on the massive derivation problem step by step in order to help readers identify and understand possible analytical solutions in their own endeavors. The stages are elementary yet rigorous; suggested student research project topics are provided. After deriving the variational equations, the authors apply them to many interesting problems, including the Earth-Moon system, the effect of an oblate planet, the perturbation of Mercury's orbit due to General Relativity, and the perturbation due to atmospheric drag. Along the way, they introduce several useful techniques such as averaging, Poincare's method of small parameters, and variation of parameters. In the end, this textbook will help students, practicing engineers, and professionals across the fields of astrodynamics, astronomy, dynamics, physics, planetary science, spacecraft missions, and others. 001444862 588__ $$aDescription based upon print version of record. 001444862 650_0 $$aPlanets$$xOrbits. 001444862 650_0 $$aPerturbation (Astronomy) 001444862 650_6 $$aPlanètes$$xOrbites. 001444862 650_6 $$aPerturbation (Astronomie) 001444862 655_0 $$aElectronic books. 001444862 7001_ $$aHoots, Felix R.,$$d1947-$$eauthor. 001444862 7001_ $$aPollock, George E.,$$eauthor. 001444862 77608 $$iPrint version:$$aLonguski, James M.$$tIntroduction to Orbital Perturbations$$dCham : Springer International Publishing AG,c2022$$z9783030897574 001444862 830_0 $$aSpace technology library ;$$vv. 40. 001444862 852__ $$bebk 001444862 85640 $$3Springer Nature$$uhttps://univsouthin.idm.oclc.org/login?url=https://link.springer.com/10.1007/978-3-030-89758-1$$zOnline Access$$91397441.1 001444862 909CO $$ooai:library.usi.edu:1444862$$pGLOBAL_SET 001444862 980__ $$aBIB 001444862 980__ $$aEBOOK 001444862 982__ $$aEbook 001444862 983__ $$aOnline 001444862 994__ $$a92$$bISE